EP0178560B1 - Support for cryostat penetration tube - Google Patents
Support for cryostat penetration tube Download PDFInfo
- Publication number
- EP0178560B1 EP0178560B1 EP19850112654 EP85112654A EP0178560B1 EP 0178560 B1 EP0178560 B1 EP 0178560B1 EP 19850112654 EP19850112654 EP 19850112654 EP 85112654 A EP85112654 A EP 85112654A EP 0178560 B1 EP0178560 B1 EP 0178560B1
- Authority
- EP
- European Patent Office
- Prior art keywords
- assembly
- affixed
- wall
- cryostat
- bearing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
Links
Images
Classifications
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C13/00—Details of vessels or of the filling or discharging of vessels
- F17C13/08—Mounting arrangements for vessels
- F17C13/086—Mounting arrangements for vessels for Dewar vessels or cryostats
- F17C13/087—Mounting arrangements for vessels for Dewar vessels or cryostats used for superconducting phenomena
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C3/00—Vessels not under pressure
- F17C3/02—Vessels not under pressure with provision for thermal insulation
- F17C3/08—Vessels not under pressure with provision for thermal insulation by vacuum spaces, e.g. Dewar flask
- F17C3/085—Cryostats
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/03—Thermal insulations
- F17C2203/0391—Thermal insulations by vacuum
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2203/00—Vessel construction, in particular walls or details thereof
- F17C2203/06—Materials for walls or layers thereof; Properties or structures of walls or their materials
- F17C2203/068—Special properties of materials for vessel walls
- F17C2203/0687—Special properties of materials for vessel walls superconducting
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2221/00—Handled fluid, in particular type of fluid
- F17C2221/01—Pure fluids
- F17C2221/016—Noble gases (Ar, Kr, Xe)
- F17C2221/017—Helium
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2223/00—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel
- F17C2223/01—Handled fluid before transfer, i.e. state of fluid when stored in the vessel or before transfer from the vessel characterised by the phase
- F17C2223/0146—Two-phase
- F17C2223/0153—Liquefied gas, e.g. LPG, GPL
- F17C2223/0161—Liquefied gas, e.g. LPG, GPL cryogenic, e.g. LNG, GNL, PLNG
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F17—STORING OR DISTRIBUTING GASES OR LIQUIDS
- F17C—VESSELS FOR CONTAINING OR STORING COMPRESSED, LIQUEFIED OR SOLIDIFIED GASES; FIXED-CAPACITY GAS-HOLDERS; FILLING VESSELS WITH, OR DISCHARGING FROM VESSELS, COMPRESSED, LIQUEFIED, OR SOLIDIFIED GASES
- F17C2270/00—Applications
- F17C2270/05—Applications for industrial use
- F17C2270/0527—Superconductors
- F17C2270/0536—Magnetic resonance imaging
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- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S220/00—Receptacles
- Y10S220/901—Liquified gas content, cryogenic
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S285/00—Pipe joints or couplings
- Y10S285/904—Cryogenic
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S505/00—Superconductor technology: apparatus, material, process
- Y10S505/825—Apparatus per se, device per se, or process of making or operating same
- Y10S505/888—Refrigeration
- Y10S505/892—Magnetic device cooling
Definitions
- the present invention is related to a penetration assembly for a cryostat construction according to the first part of claim 1 and in particular to means for supporting a thin-walled horizontal penetration tube so as to permit relative motion between inner and outer cryostat vessels without unduly stressing the pentration tube.
- the present invention is also related to the construction of cryostats for containing coolants such as liquid helium used to cool the superconductive windings of a main magnet for a medical diagnostic nuclear magnetic resonance (NMR) imaging system.
- coolants such as liquid helium used to cool the superconductive windings of a main magnet for a medical diagnostic nuclear magnetic resonance (NMR) imaging system.
- cryostats for NMR imaging systems typically require disruption of the cryostat vacuum for the purpose of inserting temporary stiffening supports to protect the magnet and internal components during transportation. Transportation of such superconducting magnets is therefore seen to require re-establishment of internal vacuum conditions after the magnet is disassembled to remove the temporary support. This is a time-consuming operation.
- large elastomer seals are commonly employed to facilitate assembly and disassembly.
- other cryostat designs have included a non-metallic cryostat bore tube wall to prevent eddy current field distortions when NMR gradient coils are energized. These gradient coils are typically disposed within the bore of the magnet assembly.
- both elastomer seals and non-metallic bore tubes are permeable to gases and either design results in contamination of the internal vacuum conditions during long term operation of the device. Therefore, periodic pumping of the cryostat is required. Morever, seal replacement requires periodic total shutdown and warming of the superconductor windings to ambient temperature conditions. Accordingly, it is seen that it is desirable to permanently maintain vacuum conditions within a cryostat, not only for purposes of transport, but also for purposes of long term operation.
- cryostats employed to house superconducting windings which are used to produce a high intensity magnetic field for whole body NMR imaging applications. Since the bore tube of the magnet assembly must be sized to accommodate the human form, with the bore tube typically being approximately one meter in diameter, the overall size of the magnet and cryostat significantly affects the cost, most notably of the magnet itself but also the cost of the room or structure in which it is housed. Accordingly, it is desired to provide a cryostat housing having horizontal access means for addition of liquid coolant and for penetration of electrical leads, these means being located at the end surface of the cryostat.
- a thin walled penetration tube is employed. Additionally, vacuum conditions are maintained between inner and outer cryostat vessels and a system of supporting ties is employed at each end of the inner vessel so as to support the inner vessel within the outer vessel. It is also noted that in these cryostat structures, intermediate vessels and thermal radiation shields are also typically present to increase the effectiveness of the cryostat.
- a system of supporting ties preferably permits axial motion so that the inner vesel may be moved axially and locked into a fixed position during transport. This permits transport of the magnet and cryostat assembly in a fully charged condition, that is, in a condition in which the magnet and coil superconductors have already been cooled to below their critical temperatures. This permits rapid system installation.
- one of the objects of the present invention is to provide a support for this relatively delicate penetration tube.
- transverse and rocking motions of the inner vessel can also occur.
- Thin walled penetration tubes fixed to both the inner and outer cryostat vessels could be subject to potentially damaging mechanical stresses as a result of the relative motion between the inner and outer cryostat vessels.
- differential thermal expansion and contraction effects can also operate to induce stress in penetration tubes which are firmly anchored to both the inner and- outer vessel walls.
- a penetration assembly for a cryostat which comprises a penetration tube affixed to an inner cryostat vessel wall and extending through an aperture in an outer cryostat vessel wall; an outer flange affixed to the exterior end of the penetration tube an airtight bellows affixed to and extending from the outer flange toward the outer wall and also being affixed relative to the outer wall so as to surround the aperture in the outer wall, a washer-shaped bearing through which said penetration tube is disposed, said bearing being disposed between said outer wall and said flange, means to hold the bearing so as to restrict its permissible motions to those lying in a plane substantially parallel to the outer wall and means to affix said outer flange to said bearing.
- the bearing is affixed to the outer flange, such as by threaded bolts disposed through radially oriented slots in the bearing hold down means.
- the bearing is preferably provided with a coated surface so as to be able to readily permit transverse motions.
- the penetration assembly is therefore seen to provide axial motion through the bellows, when desired. Trans- vere motions and rocking motions are seen to be accommodated by the combination of the bellows and the bearing assembly which functions essentially as a thrust bearing.
- cryostat penetration tube 11 extending between inner cryostat vessel wall 12 and outer cryostat vessel wall 13.
- the metallic structures preferably comprise non-megnatic alloys such as aluminum or stainless steel.
- penetration tube 11 preferably comprises stainless steel.
- transition collar 14 which preferably comprises aluminum. Collar 14 is brazed to tube 11 at one end and welded to inner vessel wall 12 as shown. Penetration tube 11 extends through aperture 22 in exterior cryostat vessel wall 13. Penetration tube 11 is welded to outer or exterior flange 15, which also preferably comprises stainless steel. Metal bellows 16 is sealably affixed to outer flange 15 so as to surround penetration tube 11 and so as to extend toward outer vessel wall 13 to which it is either directly or indirectly affixed so as to surround aperture 22. Bellows 16 provides sufficient flexibility to accommodate large transverse displacements.
- Bellows 16 may be directly affixed to exterior wall 13, but may also be affixed to circular boss 26 which is itself affixed to exterior wall 13 by means of weld joint 27.
- inner vessel wall 12, collar 14, penetration tube 11, flange 15, bellows 16, boss 26 and exterior vessel wall 13 all form part of an evacu- able volume maintained between the inner and outer cryostat vessels.
- Bolts 17 are affixed to flange 15 by any convenient means such as by nuts 24 and 25, as shown.
- One end of bolt 17 is affixed to flange 15 with the other end being affixed to split ring bearing 18 disposed between boss 26 and cup shaped retaining flange 19 which is affixed to boss 26 by any convenient means, such as by bolt 23 as shown.
- Bearing 18 is provided with a slippery coating such as polytetrafluoroethylene (PTFE).
- PTFE polytetrafluoroethylene
- Tef- lonTM and RulonTM may be employed.
- Bolts 17 are threaded directly into bearing 18.
- boss 26 together with retaining flange 19 provide a channel in which bearing 18 may undergo tranverse motions which are substantially parallel to the plane of outer vessel wall 13. Coating 21 on bearing 18 facilitates this motion and prevents binding which would induce stress in thin walled tube 11.
- bolts 17 are disposed through radially oriented slots 20 in retaining flange 19. Bearing 18 is restrained axially by retaining flange 19, but is free to move transversely so as to function as a thrust bearing. Axial clearance is provided between bearing 18 and its housing so that small rocking motions of penetration tube 11 are accommodated.
- the penetration tube assembly of the present invention permits tube motions which are desired to prevent excessive stress in the thin walled structure. It is also seen that bellows 16 permits the desired axial positioning of the inner and outer vessels and also simultaneously, in cooperation with coated thrust bearing 18, permits the desired degree of transverse and rocking motions which are particularly associated with cryostat transport. Additionally, it is seen that the penetration tube assembly of the present invention also provides means for compensating differing degrees and rates of thermal expansion between the inner and outer cryostat vessels, particularly during cryostat coolant charging operations.
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- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Thermal Sciences (AREA)
- Containers, Films, And Cooling For Superconductive Devices (AREA)
- Magnetic Resonance Imaging Apparatus (AREA)
- Filling Or Discharging Of Gas Storage Vessels (AREA)
Description
- The present invention is related to a penetration assembly for a cryostat construction according to the first part of claim 1 and in particular to means for supporting a thin-walled horizontal penetration tube so as to permit relative motion between inner and outer cryostat vessels without unduly stressing the pentration tube. The present invention is also related to the construction of cryostats for containing coolants such as liquid helium used to cool the superconductive windings of a main magnet for a medical diagnostic nuclear magnetic resonance (NMR) imaging system.
- Conventional cryostats for NMR imaging systems typically require disruption of the cryostat vacuum for the purpose of inserting temporary stiffening supports to protect the magnet and internal components during transportation. Transportation of such superconducting magnets is therefore seen to require re-establishment of internal vacuum conditions after the magnet is disassembled to remove the temporary support. This is a time-consuming operation. In conventional cryostat designs, large elastomer seals are commonly employed to facilitate assembly and disassembly. Furthermore, other cryostat designs have included a non-metallic cryostat bore tube wall to prevent eddy current field distortions when NMR gradient coils are energized. These gradient coils are typically disposed within the bore of the magnet assembly. However, both elastomer seals and non-metallic bore tubes are permeable to gases and either design results in contamination of the internal vacuum conditions during long term operation of the device. Therefore, periodic pumping of the cryostat is required. Morever, seal replacement requires periodic total shutdown and warming of the superconductor windings to ambient temperature conditions. Accordingly, it is seen that it is desirable to permanently maintain vacuum conditions within a cryostat, not only for purposes of transport, but also for purposes of long term operation.
- Conventional cyrostat designs also typically employ an access port for addition of coolants such as liquid helium in awkward positions on top of the cylindrical cryostat structure. Such coolant access means are conventionally disposed on the curved side surface of the cryostat and adds significantly to the overall dimensions of the cryostat assembly. This is a significant disadvantage for cryostats employed to house superconducting windings which are used to produce a high intensity magnetic field for whole body NMR imaging applications. Since the bore tube of the magnet assembly must be sized to accommodate the human form, with the bore tube typically being approximately one meter in diameter, the overall size of the magnet and cryostat significantly affects the cost, most notably of the magnet itself but also the cost of the room or structure in which it is housed. Accordingly, it is desired to provide a cryostat housing having horizontal access means for addition of liquid coolant and for penetration of electrical leads, these means being located at the end surface of the cryostat.
- In order to minimize thermal conduction between inner and outer cryostat vessel walls, a thin walled penetration tube is employed. Additionally, vacuum conditions are maintained between inner and outer cryostat vessels and a system of supporting ties is employed at each end of the inner vessel so as to support the inner vessel within the outer vessel. It is also noted that in these cryostat structures, intermediate vessels and thermal radiation shields are also typically present to increase the effectiveness of the cryostat. However, a system of supporting ties preferably permits axial motion so that the inner vesel may be moved axially and locked into a fixed position during transport. This permits transport of the magnet and cryostat assembly in a fully charged condition, that is, in a condition in which the magnet and coil superconductors have already been cooled to below their critical temperatures. This permits rapid system installation.
- However, relative motion of the inner and outer cryostat vessels can severely stress the thin walled penetration tube. Accordingly, one of the objects of the present invention is to provide a support for this relatively delicate penetration tube. In addition to axial motion which is deliberately employed for purposes of transport to lock the inner cryostat vessel in a fixed position, transverse and rocking motions of the inner vessel can also occur. Thin walled penetration tubes fixed to both the inner and outer cryostat vessels could be subject to potentially damaging mechanical stresses as a result of the relative motion between the inner and outer cryostat vessels. Additionally, differential thermal expansion and contraction effects can also operate to induce stress in penetration tubes which are firmly anchored to both the inner and- outer vessel walls. The large transverse displacements and rocking motions of the inner vessel during shipment could subject the thin walled penetration tube to high bending stresses beyond yield strength. Additionally, this tube must also withstand axial loads as a result of the cryostat vacuum and magnetic interactions with external ferromagnetic objects.
- Accordingly, it is an object of the present invention to provide support means for a thin walled cryostat penetration tube.
- It is an additional object of the present invention to provide a penetration support structure which preserves internal vacuum conditions.
- It is also an object of the present invention to provide a penetration tube between inner and outer cryostat vessels which exhibits low levels of thermal conductivity.
- Lastly, but not limited hereto, it is an object of the present invention to prevent high bending stresses from occurring in cryostat penetration tubes.
- In accordance with the present invention as claimed, a penetration assembly for a cryostat is provided which comprises a penetration tube affixed to an inner cryostat vessel wall and extending through an aperture in an outer cryostat vessel wall; an outer flange affixed to the exterior end of the penetration tube an airtight bellows affixed to and extending from the outer flange toward the outer wall and also being affixed relative to the outer wall so as to surround the aperture in the outer wall, a washer-shaped bearing through which said penetration tube is disposed, said bearing being disposed between said outer wall and said flange, means to hold the bearing so as to restrict its permissible motions to those lying in a plane substantially parallel to the outer wall and means to affix said outer flange to said bearing. The bearing is affixed to the outer flange, such as by threaded bolts disposed through radially oriented slots in the bearing hold down means. The bearing is preferably provided with a coated surface so as to be able to readily permit transverse motions. The penetration assembly is therefore seen to provide axial motion through the bellows, when desired. Trans- vere motions and rocking motions are seen to be accommodated by the combination of the bellows and the bearing assembly which functions essentially as a thrust bearing.
- The subject matter which is regarded as the invention is particularly pointed out and distinctly claimed in the concluding portion of the specification. The invention, however, both as to organization and method of practice, together with further objects and advantages thereof may best be understood by reference of the following description taken in connection with the accompanying drawing in which:
- The Figure is a cross-sectional side elevation of a cryostat penetration assembly in accordance with the present invention particularly illustrating a penetration tube extending between an inner and an outer cryostat vessel wall.
- The Figure illustrates, in cross-section, cryostat penetration tube 11 extending between inner
cryostat vessel wall 12 and outercryostat vessel wall 13. Throughout the Figure all structures shown are metallic except forcoating 21 on bearing 18. In particular, the metallic structures preferably comprise non-megnatic alloys such as aluminum or stainless steel. In particular, penetration tube 11 preferably comprises stainless steel. - At the inner or cold end of penetration tube 11, it is joined to inner
cryostat vessel wall 12 by means oftransition collar 14 which preferably comprises aluminum.Collar 14 is brazed to tube 11 at one end and welded toinner vessel wall 12 as shown. Penetration tube 11 extends throughaperture 22 in exteriorcryostat vessel wall 13. Penetration tube 11 is welded to outer orexterior flange 15, which also preferably comprises stainless steel.Metal bellows 16 is sealably affixed toouter flange 15 so as to surround penetration tube 11 and so as to extend towardouter vessel wall 13 to which it is either directly or indirectly affixed so as to surroundaperture 22. Bellows 16 provides sufficient flexibility to accommodate large transverse displacements. Bellows 16 may be directly affixed toexterior wall 13, but may also be affixed tocircular boss 26 which is itself affixed toexterior wall 13 by means ofweld joint 27. In particular,inner vessel wall 12,collar 14, penetration tube 11,flange 15,bellows 16,boss 26 andexterior vessel wall 13 all form part of an evacu- able volume maintained between the inner and outer cryostat vessels. - Bolts 17 (one shown) are affixed to
flange 15 by any convenient means such as bynuts bolt 17 is affixed toflange 15 with the other end being affixed to split ring bearing 18 disposed betweenboss 26 and cup shapedretaining flange 19 which is affixed toboss 26 by any convenient means, such as by bolt 23 as shown.Bearing 18 is provided with a slippery coating such as polytetrafluoroethylene (PTFE). For this purpose, materials such as Tef- lon™ and RulonTM may be employed.Bolts 17 are threaded directly intobearing 18. It is also seen thatboss 26 together with retainingflange 19 provide a channel in which bearing 18 may undergo tranverse motions which are substantially parallel to the plane ofouter vessel wall 13.Coating 21 on bearing 18 facilitates this motion and prevents binding which would induce stress in thin walled tube 11. Additionally, it is seen thatbolts 17 are disposed through radially orientedslots 20 in retainingflange 19.Bearing 18 is restrained axially by retainingflange 19, but is free to move transversely so as to function as a thrust bearing. Axial clearance is provided betweenbearing 18 and its housing so that small rocking motions of penetration tube 11 are accommodated. - From the above, it should be appreciated that the penetration tube assembly of the present invention permits tube motions which are desired to prevent excessive stress in the thin walled structure. It is also seen that bellows 16 permits the desired axial positioning of the inner and outer vessels and also simultaneously, in cooperation with
coated thrust bearing 18, permits the desired degree of transverse and rocking motions which are particularly associated with cryostat transport. Additionally, it is seen that the penetration tube assembly of the present invention also provides means for compensating differing degrees and rates of thermal expansion between the inner and outer cryostat vessels, particularly during cryostat coolant charging operations.
Claims (12)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US661013 | 1984-10-15 | ||
US06/661,013 US4526015A (en) | 1984-10-15 | 1984-10-15 | Support for cryostat penetration tube |
Publications (2)
Publication Number | Publication Date |
---|---|
EP0178560A1 EP0178560A1 (en) | 1986-04-23 |
EP0178560B1 true EP0178560B1 (en) | 1988-08-17 |
Family
ID=24651841
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
EP19850112654 Expired EP0178560B1 (en) | 1984-10-15 | 1985-10-07 | Support for cryostat penetration tube |
Country Status (7)
Country | Link |
---|---|
US (1) | US4526015A (en) |
EP (1) | EP0178560B1 (en) |
JP (1) | JPS6196299A (en) |
CN (1) | CN1004223B (en) |
CA (1) | CA1258663A (en) |
DE (1) | DE3564478D1 (en) |
IL (1) | IL76253A0 (en) |
Families Citing this family (55)
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DE3632490A1 (en) * | 1985-09-24 | 1987-04-02 | Mitsubishi Electric Corp | HEAT-INSULATING CARRIER |
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GB1008740A (en) * | 1959-02-20 | 1965-11-03 | Secr Aviation | Refrigeration unit |
US3066222A (en) * | 1959-11-18 | 1962-11-27 | Union Carbide Corp | Infra-red detection apparatus |
US3423955A (en) * | 1966-06-08 | 1969-01-28 | Andonian Associates Inc | Flexible cold finger for cooling samples to cryogenic temperatures |
US3483709A (en) * | 1967-07-21 | 1969-12-16 | Princeton Gamma Tech Inc | Low temperature system |
DE2806829C3 (en) * | 1978-02-17 | 1984-09-20 | Deutsche Forschungs- Und Versuchsanstalt Fuer Luft- Und Raumfahrt E.V., 5000 Koeln | Device for deep freezing of objects |
JPS5787185A (en) * | 1980-11-19 | 1982-05-31 | Hitachi Ltd | Crygenic device |
JPS57143496U (en) * | 1981-03-04 | 1982-09-08 | ||
US4522034A (en) * | 1984-03-30 | 1985-06-11 | General Electric Company | Horizontal cryostat penetration insert and assembly |
-
1984
- 1984-10-15 US US06/661,013 patent/US4526015A/en not_active Expired - Fee Related
-
1985
- 1985-06-20 CA CA000484610A patent/CA1258663A/en not_active Expired
- 1985-08-29 IL IL76253A patent/IL76253A0/en not_active IP Right Cessation
- 1985-09-05 CN CN85106738.7A patent/CN1004223B/en not_active Expired
- 1985-10-03 JP JP60219298A patent/JPS6196299A/en active Granted
- 1985-10-07 EP EP19850112654 patent/EP0178560B1/en not_active Expired
- 1985-10-07 DE DE8585112654T patent/DE3564478D1/en not_active Expired
Also Published As
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---|---|
JPH0418189B2 (en) | 1992-03-27 |
JPS6196299A (en) | 1986-05-14 |
EP0178560A1 (en) | 1986-04-23 |
IL76253A0 (en) | 1986-01-31 |
CA1258663A (en) | 1989-08-22 |
US4526015A (en) | 1985-07-02 |
DE3564478D1 (en) | 1988-09-22 |
CN85106738A (en) | 1986-06-10 |
CN1004223B (en) | 1989-05-17 |
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